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Abstract

We describe the cryogenic system being developed for Taurus: a super-pressure balloon-borne microwave polarimeter scheduled to fly in 2027. The Taurus cryogenic system consists of a 660L liquid helium cryostat which achieves a base temperature of <100mK with the help of a capillary-fed superfluid tank and a closed cycle dilution refrigerator. The main tank is supported with fiberglass flexures and is encased in two layers of vapor-cooled shields which allow Taurus to make full use of the extended flight time offered by the super-pressure balloon platform. The Taurus cryostat is projected to hold for over 50 days while weighing under 1000lbs. We present the design, testing, and thermal analysis of the Taurus cryogenic systems.

Details

1009240
Title
Thermal architecture for a cryogenic super-pressure balloon payload: design and development of the Taurus flight cryostat
Publication title
arXiv.org; Ithaca
Publication year
2024
Publication date
Oct 23, 2024
Section
Astrophysics; Physics (Other)
Publisher
Cornell University Library, arXiv.org
Source
arXiv.org
Place of publication
Ithaca
Country of publication
United States
University/institution
Cornell University Library arXiv.org
e-ISSN
2331-8422
Source type
Working Paper
Language of publication
English
Document type
Working Paper
Publication history
 
 
Online publication date
2024-10-25
Milestone dates
2024-10-23 (Submission v1)
Publication history
 
 
   First posting date
25 Oct 2024
ProQuest document ID
3120693865
Document URL
https://www.proquest.com/working-papers/thermal-architecture-cryogenic-super-pressure/docview/3120693865/se-2?accountid=208611
Full text outside of ProQuest
Copyright
© 2024. This work is published under http://creativecommons.org/licenses/by-nc-sa/4.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.
Last updated
2024-10-26
Database
ProQuest One Academic